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Airbus A321
First flight year — 1993
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Airbus A321 Specifications
| A321-100/200 | |
| Dimensions | |
| Length (m) | 44.5 |
| Wingspan (m) | 34.1 |
| Height (m) | 11.8 |
| Wing area (m2) | 122.4 |
| Weight | |
| Maximum take-off weight (kg) | 83 000 - 93 500 |
| Maximum landing weight (kg) | 73 500 - 77 800 |
| Operating empty weight (kg) | 48 100 |
| Maximum zero fuel weight (kg) | 71 500 |
| Maximum payload (kg) | 23 400 |
| Standard fuel capacity (litres) | 23 700 - 29 680 |
| Performance | |
| Range with max payload (km) | 5 000 - 5 500 |
| Maximum cruise speed (km/h) | 840 |
| Maximum cruise speed (km/h) | 890 |
| Maximum operating altitude (km) | 11 900 |
| Take-off field length (m) | 2 180 |
| Landing field length (m) | 1 580 |
| Engines | CFMI CFM56-5A/5B, 2 x 30000-33000 lbIAE V2500-A5, 2 x 30000-33000 lb |
| Fuel efficiency (g/pass*km) | 18.2 |
| Fuel flow rate (kg/h) | 3 200 |
| Cabin Data | |
| Passengers (1-class) | 220 |
| Passengers (2-class) | 185 |
| Cabin width (m) | 3.7 |
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